Investigation of separation control in compressible boundary layers using periodic disturbances

Daniel M. Israel, Hermann F Fasel

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Scopus citations

Abstract

The effect of compressibility on flow control by periodic blowing and suction in an adverse pressure gradient boundary layer is studied using direct numerical simulation based on the two- dimensional compressible Navier-Stokes equations. Previous work has shown that oscillating disturbances can reduce or eliminate separation, as well as weakening buffeting downstream of the separated region, both for separation bubbles and for massively separated flows. We examine the flow field for two Reynolds numbers, and for Mach numbers Ma = 0.3 and 0.6. For the low Reynolds number case we examine the development of instability waves, and show that their behavior can be modified by periodic forcing. For the high Reynolds number, the flow strongly separates and we show that flow control by periodic disturbances is effective at both Mach numbers.

Original languageEnglish (US)
Title of host publication30th Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9780000000002
StatePublished - 1999
Event30th Fluid Dynamics Conference, 1999 - Norfolk, United States
Duration: Jun 28 1999Jul 1 1999

Other

Other30th Fluid Dynamics Conference, 1999
CountryUnited States
CityNorfolk
Period6/28/997/1/99

ASJC Scopus subject areas

  • Engineering(all)

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    Israel, D. M., & Fasel, H. F. (1999). Investigation of separation control in compressible boundary layers using periodic disturbances. In 30th Fluid Dynamics Conference [AIAA 99-3657] American Institute of Aeronautics and Astronautics Inc, AIAA.